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Attributes | |
ACN | 681870 |
Time | |
Date | 200512 |
Local Time Of Day | 1801 To 2400 |
Place | |
Locale Reference | airport : zzz.airport |
State Reference | US |
Altitude | agl single value : 0 |
Environment | |
Light | Night |
Aircraft 1 | |
Operator | common carrier : air carrier |
Make Model Name | B737-700 |
Operating Under FAR Part | Part 121 |
Flight Phase | ground : parked ground : maintenance |
Flight Plan | IFR |
Person 1 | |
Affiliation | company : air carrier |
Function | flight crew : captain oversight : pic |
Experience | flight time last 90 days : 275 flight time total : 10600 flight time type : 6500 |
ASRS Report | 681870 |
Person 2 | |
Affiliation | company : air carrier |
Function | flight crew : first officer |
Experience | flight time last 90 days : 200 flight time total : 4000 flight time type : 350 |
ASRS Report | 681964 |
Events | |
Anomaly | aircraft equipment problem : critical maintenance problem : non compliance with mel non adherence : far non adherence : published procedure |
Independent Detector | aircraft equipment other aircraft equipment : volt meter inverter test other flight crewa other flight crewb |
Resolutory Action | none taken : detected after the fact |
Consequence | other |
Factors | |
Maintenance | contributing factor : schedule pressure contributing factor : manuals performance deficiency : fault isolation performance deficiency : logbook entry performance deficiency : non compliance with legal requirements performance deficiency : repair performance deficiency : testing |
Supplementary | |
Problem Areas | Environmental Factor Maintenance Human Performance Aircraft Chart Or Publication |
Primary Problem | Maintenance Human Performance |
Situations | |
Publication | Minimum Equipment List |
Narrative:
We received our aircraft in ZZZ approximately 4 hours late. The aircraft had MEL 24-16 inoperative elec light dated several days prior. The MEL had two provisos; 1ST; a standby powered check done at the time of deferral and 2ND a check of the battery charger prior to flight using the procedure spelled out in the MEL. We completed our preflight and also did the battery charger check. It went as published. En route during my cruise flow I was checking the elec panel and noticed that the inv on the AC side was un-powered. When we arrived at our destination; I called maintenance control to talk to them about the write-up in the logbook concerning the MEL and the deferral. The deferral stated nothing about the standby powered check being completed when the elec light was deferred. This was not a specific maintenance procedure but just a proviso in the MEL. The first officer and I decided to do a standby powered check just for our own comfort. We used the standby powered check for -700 aircraft that was in the MEL. The test failed. The AC standby bus was unpowered. I then called maintenance control back and we ran thru another check and decided that the AC standby bus was not powered. I wrote the aircraft up and we were assigned a new aircraft. The original MEL deferral said that at startup; the elec light illuminated. The signoff was a very simple 'ok to continue per MEL 24-16.' I was signed off by a mechanic. It is my thinking that at the time of the deferral; the standby powered check was not done but the battery charger check was. If this were the case then this aircraft flew for several days without an operating AC standby bus. I would recommend that as a part of this MEL; a procedure be put in place to require a standby powered check prior to the first flight of each day.callback conversation with reporter revealed the following information: the reporter stated the 'elec' annunciator light was deferred per the minimum equipment list and it was obvious the required special procedure check of the standby powered test was not accomplished at the time of deferral. The reporter indicated the only minimum equipment list special procedure required by the flight crew was a check of the battery charger and not a standby powered check. Reporter suggested this be changed to add a battery charger and not a standby powered check prior to flight with this minimum equipment list deferral. Reportedly this airplane was operated for several days with the AC standby inverter inoperative.
Original NASA ASRS Text
Title: A B737-700 WAS DISPATCHED WITH AN 'ELEC' ANNUNCIATOR LIGHT DEFERRED PER THE MEL. THE ACFT WAS UNKNOWINGLY OPERATED WITH AN AC STANDBY BUS THAT COULD NOT BE POWERED FROM THE BATTERY. RPTR RECOMMENDS MEL SPECIAL PROC REQUIRE FLT CREW TO CONDUCT STANDBY POWER CHK PRIOR TO DAILY FLT.
Narrative: WE RECEIVED OUR ACFT IN ZZZ APPROX 4 HRS LATE. THE ACFT HAD MEL 24-16 INOP ELEC LIGHT DATED SEVERAL DAYS PRIOR. THE MEL HAD TWO PROVISOS; 1ST; A STANDBY POWERED CHK DONE AT THE TIME OF DEFERRAL AND 2ND A CHK OF THE BATTERY CHARGER PRIOR TO FLT USING THE PROC SPELLED OUT IN THE MEL. WE COMPLETED OUR PREFLT AND ALSO DID THE BATTERY CHARGER CHECK. IT WENT AS PUBLISHED. ENRTE DURING MY CRUISE FLOW I WAS CHKING THE ELEC PANEL AND NOTICED THAT THE INV ON THE AC SIDE WAS UN-POWERED. WHEN WE ARRIVED AT OUR DEST; I CALLED MAINT CTL TO TALK TO THEM ABOUT THE WRITE-UP IN THE LOGBOOK CONCERNING THE MEL AND THE DEFERRAL. THE DEFERRAL STATED NOTHING ABOUT THE STANDBY POWERED CHK BEING COMPLETED WHEN THE ELEC LIGHT WAS DEFERRED. THIS WAS NOT A SPECIFIC MAINT PROC BUT JUST A PROVISO IN THE MEL. THE FO AND I DECIDED TO DO A STANDBY POWERED CHK JUST FOR OUR OWN COMFORT. WE USED THE STANDBY POWERED CHK FOR -700 ACFT THAT WAS IN THE MEL. THE TEST FAILED. THE AC STANDBY BUS WAS UNPOWERED. I THEN CALLED MAINT CTL BACK AND WE RAN THRU ANOTHER CHK AND DECIDED THAT THE AC STANDBY BUS WAS NOT POWERED. I WROTE THE ACFT UP AND WE WERE ASSIGNED A NEW ACFT. THE ORIGINAL MEL DEFERRAL SAID THAT AT STARTUP; THE ELEC LIGHT ILLUMINATED. THE SIGNOFF WAS A VERY SIMPLE 'OK TO CONTINUE PER MEL 24-16.' I WAS SIGNED OFF BY A MECH. IT IS MY THINKING THAT AT THE TIME OF THE DEFERRAL; THE STANDBY POWERED CHK WAS NOT DONE BUT THE BATTERY CHARGER CHK WAS. IF THIS WERE THE CASE THEN THIS ACFT FLEW FOR SEVERAL DAYS WITHOUT AN OPERATING AC STANDBY BUS. I WOULD RECOMMEND THAT AS A PART OF THIS MEL; A PROC BE PUT IN PLACE TO REQUIRE A STANDBY POWERED CHK PRIOR TO THE FIRST FLT OF EACH DAY.CALLBACK CONVERSATION WITH RPTR REVEALED THE FOLLOWING INFO: THE RPTR STATED THE 'ELEC' ANNUNCIATOR LIGHT WAS DEFERRED PER THE MINIMUM EQUIPMENT LIST AND IT WAS OBVIOUS THE REQUIRED SPECIAL PROC CHK OF THE STANDBY POWERED TEST WAS NOT ACCOMPLISHED AT THE TIME OF DEFERRAL. THE RPTR INDICATED THE ONLY MINIMUM EQUIPMENT LIST SPECIAL PROC REQUIRED BY THE FLT CREW WAS A CHK OF THE BATTERY CHARGER AND NOT A STANDBY POWERED CHECK. RPTR SUGGESTED THIS BE CHANGED TO ADD A BATTERY CHARGER AND NOT A STANDBY POWERED CHK PRIOR TO FLT WITH THIS MINIMUM EQUIPMENT LIST DEFERRAL. REPORTEDLY THIS AIRPLANE WAS OPERATED FOR SEVERAL DAYS WITH THE AC STANDBY INVERTER INOP.
Data retrieved from NASA's ASRS site as of January 2009 and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.